Study on interception control strategies with zero effort miss

Zhongcheng Mu; Jinling Qi; Dong Ye; Keke Zhang

doi:10.1109/CCDC.2017.7978980

Study on interception control strategies with zero effort miss

Zhongcheng Mu
, Jinling Qi
, Dong Ye
, Keke Zhang

School of Instrumentation Science and Engineering

Shanghai Engineering Center for Microsatellites
CAS - Shanghai Institute of Microsystem and Information Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

In the present paper the terminal orbital control in the satellite pursuit-evasion game was studied, where the orbital maneuver with using limited magnitude continuous thrust was involved for both the interceptor and target. Since considering the terminal application scenario the high nonlinear interception dynamics could be reduced to the CW equations. Based on the reduced CW equation, zero effort miss was proposed to obtain the orbit control strategy. And with adding the fuel consumption the controller was built. Finally, the proposed method was validated by the numerical simulation, and the advantage and weakness of the proposed control strategy was analyzed.

Original language	English
Title of host publication	Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	2747-2754
Number of pages	8
ISBN (Electronic)	9781509046560
DOIs	https://doi.org/10.1109/CCDC.2017.7978980
State	Published - 12 Jul 2017
Event	29th Chinese Control and Decision Conference, CCDC 2017 - Chongqing, China Duration: 28 May 2017 → 30 May 2017

Publication series

Name	Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017

Conference

Conference	29th Chinese Control and Decision Conference, CCDC 2017
Country/Territory	China
City	Chongqing
Period	28/05/17 → 30/05/17

Keywords

Pursuit-evasion game
Reduced CW equation
Zero Effort Miss optimal Control

Access to Document

10.1109/CCDC.2017.7978980

Cite this

Mu, Z., Qi, J., Ye, D., & Zhang, K. (2017). Study on interception control strategies with zero effort miss. In Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017 (pp. 2747-2754). Article 7978980 (Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CCDC.2017.7978980

@inproceedings{57159994c4fe436e8aedde92c52cb4e6,

title = "Study on interception control strategies with zero effort miss",

abstract = "In the present paper the terminal orbital control in the satellite pursuit-evasion game was studied, where the orbital maneuver with using limited magnitude continuous thrust was involved for both the interceptor and target. Since considering the terminal application scenario the high nonlinear interception dynamics could be reduced to the CW equations. Based on the reduced CW equation, zero effort miss was proposed to obtain the orbit control strategy. And with adding the fuel consumption the controller was built. Finally, the proposed method was validated by the numerical simulation, and the advantage and weakness of the proposed control strategy was analyzed.",

keywords = "Pursuit-evasion game, Reduced CW equation, Zero Effort Miss optimal Control",

author = "Zhongcheng Mu and Jinling Qi and Dong Ye and Keke Zhang",

note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 29th Chinese Control and Decision Conference, CCDC 2017 ; Conference date: 28-05-2017 Through 30-05-2017",

year = "2017",

month = jul,

day = "12",

doi = "10.1109/CCDC.2017.7978980",

language = "英语",

series = "Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

pages = "2747--2754",

booktitle = "Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017",

address = "美国",

}

Mu, Z, Qi, J, Ye, D & Zhang, K 2017, Study on interception control strategies with zero effort miss. in Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017., 7978980, Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017, Institute of Electrical and Electronics Engineers Inc., pp. 2747-2754, 29th Chinese Control and Decision Conference, CCDC 2017, Chongqing, China, 28/05/17. https://doi.org/10.1109/CCDC.2017.7978980

Study on interception control strategies with zero effort miss. / Mu, Zhongcheng; Qi, Jinling; Ye, Dong et al.
Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017. Institute of Electrical and Electronics Engineers Inc., 2017. p. 2747-2754 7978980 (Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Study on interception control strategies with zero effort miss

AU - Mu, Zhongcheng

AU - Qi, Jinling

AU - Ye, Dong

AU - Zhang, Keke

PY - 2017/7/12

Y1 - 2017/7/12

N2 - In the present paper the terminal orbital control in the satellite pursuit-evasion game was studied, where the orbital maneuver with using limited magnitude continuous thrust was involved for both the interceptor and target. Since considering the terminal application scenario the high nonlinear interception dynamics could be reduced to the CW equations. Based on the reduced CW equation, zero effort miss was proposed to obtain the orbit control strategy. And with adding the fuel consumption the controller was built. Finally, the proposed method was validated by the numerical simulation, and the advantage and weakness of the proposed control strategy was analyzed.

AB - In the present paper the terminal orbital control in the satellite pursuit-evasion game was studied, where the orbital maneuver with using limited magnitude continuous thrust was involved for both the interceptor and target. Since considering the terminal application scenario the high nonlinear interception dynamics could be reduced to the CW equations. Based on the reduced CW equation, zero effort miss was proposed to obtain the orbit control strategy. And with adding the fuel consumption the controller was built. Finally, the proposed method was validated by the numerical simulation, and the advantage and weakness of the proposed control strategy was analyzed.

KW - Pursuit-evasion game

KW - Reduced CW equation

KW - Zero Effort Miss optimal Control

UR - https://www.scopus.com/pages/publications/85028040487

U2 - 10.1109/CCDC.2017.7978980

DO - 10.1109/CCDC.2017.7978980

M3 - 会议稿件

AN - SCOPUS:85028040487

T3 - Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017

SP - 2747

EP - 2754

BT - Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 29th Chinese Control and Decision Conference, CCDC 2017

Y2 - 28 May 2017 through 30 May 2017

ER -

Study on interception control strategies with zero effort miss

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